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%----------------------------------------------------------------------------- % exa060701_3.m , for example 6.7.1 and 6.5.1 % to test butter.m %---------------------------------------------------

%----------------------------------------------------------------------------- % exa060701_2.m , for example 6.7.1 and 6.5.1 % to test buttord,lp2lp,bilinear ; % to design Low-pass DF with s=2/Ts[(

%------------------------------------------------------------------------ % exa100800_corrcoef.m, % to test corrcoef.m ; %------------------------------------------------------------------------

%sjbh.m function sjbh1(m) x=-1:0.01:10; y1=sin(x); plot(x,y1) axis([-1 10 -2 2]) grid legend('sin(x)') pause(2) legend off legend('将y=sin(x)的横坐标收缩至原来的1/2') %hold on %theax=axis; pause %y

%sjbh.m %function sjbh1(m) x=-1:0.01:10; y1=sin(x); plot(x,y1) axis([-1 10 -2 2]) grid legend('sin(x)') pause(2) legend off legend('将y=sin(x)的横坐标收缩至原来的1/2') %hold on %theax=axis; pause %

%sjbh.m function sjbh1(m) x=-1:0.01:10; y1=sin(x); plot(x,y1) axis([-1 10 -2 2]) grid legend('sin(x)') pause(2) legend off legend('将y=sin(x)的横坐标收缩至原来的1/2') %hold on %theax=axis; pause %y

#include "stdio.h" #include "13kfft.c" #include "math.h" main() { int i,j; double pr[64],pi[64],fr[64],fi[64]; for (i=0; i

%Flight Simulator Servo System clear all; close all; J=2; b=0.5; kv=2; kp=15; kd=6; f1=(b+kd*kv); f2=J; F=1; A=1; t=[0:0.001:10]'; %Simulation time r=A*sin(2*pi*F*t); dr=2*pi

%S-function for continuous state equation function [sys,x0,str,ts]=s_function(t,x,u,flag) switch flag, %Initialization case 0, [sys,x0,str,ts]=mdlInitializeSizes; case 1, sys=mdlDer

function [sys,x0,str,ts] = spacemodel(t,x,u,flag) switch flag, case 0, [sys,x0,str,ts]=mdlInitializeSizes; case 1, sys=mdlDerivatives(t,x,u); case 3, sys=mdlOutputs(t,x,u); case